Avionics and Autocontrol

A New Inflation Integrity Monitoring Algorithm for Improving Availability of LAAS Signal-in-Space

Expand
  • College of Automation, Harbin Engineering University, Harbin 150001, China

Received date: 2010-06-12

  Revised date: 2010-11-11

  Online published: 2011-04-25

Abstract

The non-zero mean Gaussian error and the non-Gaussian error contained in the differential corrections which are broadcast from the local area augmentation system (LAAS) local ground facility (LGF) pose a strong threat to the integrity monitoring of signal-in-space. This paper advances an algorithm in which the mean inflation and non-Gaussian inflation are combined to improve the traditional sigma inflation. By selecting the appropriate inflation coefficients, the proposed method is not only able to overbound the tails of predefined errors, but also enhance effectively the LAAS availability level. Computer simulation results indicate that compared with the sigma inflation scheme, the availability level can be as high as 99.99% in the case of a fault-free satellite. Even in the case of a critical satellite failure, the availability benefit of the algorithm could be improved 18.97% and the availability level could be raised to 95.24%.

Cite this article

LI Liang, ZHAO Lin, DING Jicheng, GAO Shuaihe . A New Inflation Integrity Monitoring Algorithm for Improving Availability of LAAS Signal-in-Space[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011 , 32(4) : 664 -671 . DOI: CNKI:11-1929/V.20110120.1725.000

References

[1] Walter T, Enge P, Blanch J, et al. Worldwide vertical guidance of aircraft based on modernized GPS and new integrity augmentations[J]. Proceedings of the IEEE, 2008, 96(12): 1918-1935.

[2] Lee J, Pullen S, Enge P. Sigma overbounding using a position domain method for the local area augmentation of GPS[J]. IEEE Transactions on Aerospace and Electrical Systems, 2009, 45(4): 1262-1273.

[3] 甘兴利. GPS局域增强系统的完善性监测技术研究. 哈尔滨:哈尔滨工程大学自动化学院, 2008. Gan Xingli. Research on the integrity monitoring of GPS local area augmentation system. Harbin: College of Automation, Harbin Engineering University, 2008. (in Chinese)

[4] Rife J, Pullen S, Pervan B, et al. Paired overbounding and application to GPS augmentation// Position Location and Navigation Symposium. 2004: 439-446.

[5] Khanafseh S, Pervan B. Overbounding non-zero mean Gaussian ranging error for navigation integrity of LAAS//Proceedings of 2nd International Conference on Recent Advances in Space Technologies. 2005: 404-410.

[6] Khanafseh S, Pervan B. LAAS ranging error overbound for non-zero mean and non-Gaussian multipath error distributions//Proceedings of the ION 59th Annual Meeting and CIGTF 22nd Guidance Test Symposium. 2003: 490-499.

[7] Ober P B, Harriman D. On the use of multiconstellation-RAIM for aircraft approaches//Proceedings of ION GNSS 2006. 2006: 2587-2596.

[8] Murphy T, Imrich T. Implementation and operational use of ground-based augmentation systems—a component of future air traffic management system[J]. Proceedings of IEEE, 2008, 96(12): 1936-1957.

[9] DeCleene B. Defining pseudorange integrity-overbounding//Proceedings of the 13th International Technical Meeting of the Satellite Division of the Institute of Navigation. 2000: 1916-1924.

[10] Rife J, Pullen S. The impact of measurement biases on availability for CAT III LAAS[J]. Journal of The Institute of Navigation, 2005, 52(4): 215-228.

[11] Blanch J, Walter T, Enge P. Position error bound calculation for GNSS using measurement residuals[J]. IEEE Transactions on Aerospace and Electrical Systems, 2008, 44(3): 977-984.

[12] Rife J, Phelts R E. Formulation of a time-varying maximum allowable error for ground-based augmentation systems[J]. IEEE Transactions on Aerospace and Electrical Systems, 2008, 44(2): 548-559.

[13] Ene A. Further development of Galileo-GPS RAIM for vertical guidance//Proceedings of ION GNSS 2006. 2006: 2597-2607.
Outlines

/